EP0082321B1 - Flexible fibre-reinforced plastic spring and press for its manufacture - Google Patents

Flexible fibre-reinforced plastic spring and press for its manufacture Download PDF

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Publication number
EP0082321B1
EP0082321B1 EP82110755A EP82110755A EP0082321B1 EP 0082321 B1 EP0082321 B1 EP 0082321B1 EP 82110755 A EP82110755 A EP 82110755A EP 82110755 A EP82110755 A EP 82110755A EP 0082321 B1 EP0082321 B1 EP 0082321B1
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EP
European Patent Office
Prior art keywords
spring
die
intermediate layer
cheek
fibre
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
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EP82110755A
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German (de)
French (fr)
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EP0082321A2 (en
EP0082321A3 (en
Inventor
Walter Dipl.-Ing. Oefner
Franz Drachenberg
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Airbus Defence and Space GmbH
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Messerschmitt Bolkow Blohm AG
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Publication of EP0082321A3 publication Critical patent/EP0082321A3/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0003Producing profiled members, e.g. beams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/083Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60GVEHICLE SUSPENSION ARRANGEMENTS
    • B60G11/00Resilient suspensions characterised by arrangement, location or kind of springs
    • B60G11/02Resilient suspensions characterised by arrangement, location or kind of springs having leaf springs only
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/366Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers made of fibre-reinforced plastics, i.e. characterised by their special construction from such materials
    • F16F1/368Leaf springs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00Layered products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/774Springs

Definitions

  • the invention relates to a spiral spring according to the preamble of claim 1 and its manufacture.
  • the spring thickness changes are achieved by a corresponding fiber structure of the spacer layer.
  • the fibers of the spacer layer do not necessarily have to be unidirectionally oriented, but can also have a haphazard orientation, corresponding to the spiral spring known from EP-A-5 916.
  • the functional purpose of the spacer layer to ensure equal spring tensions in the spring cover layers over the entire length of the spring, is also achieved by using fiber tissue.
  • the invention is therefore based on the object, in the case of a spiral spring of the type mentioned, to be able to introduce bores for the application of force only in the finished spring base body without reducing the strength of the cover layers; moreover, a device which simplifies the production of such a spiral spring is to be shown.
  • the first part of this task is solved according to the characterizing part of patent claim 1, i.e. by a possibility of restricting spring connection bores to the spacer layer while structuring the same in such a way that these bores have a much less strength-reducing effect than with unidirectional fiber structures or structures deviating therefrom without a specific fiber orientation .
  • This is because the proposed crosswise fiber orientation allows the spacer layer to be stressed by both the longitudinal and transverse forces. In this way, the perforation reveal pressures that occur can be optimally absorbed by the spacer layer or they can be designed accordingly.
  • the second part of the above object is achieved by a press tool according to claim 3.
  • This not only has the advantage of an insertion option for a preformed spacer layer while securing the same against displacement during pressing with the cover layers (which can be produced in the pressing tool, for example, by the winding method).
  • the cover layers which can be produced in the pressing tool, for example, by the winding method.
  • the simplest measures (characterized in subclaim 4) ensure that there is no displacement of fiber strands into the joints between the upper and lower cheek parts when the pressing tool is closed. This ensures precise spring production in the dimensions required.
  • the curved leaf spring shown in Fig. 1 with a decreasing thickness from the center to both ends is a laminated body made of fiber composite material.
  • two cover layers 1, 2 of glass or similar fiber strands embedded in a resin or similar binding compound are connected in unidirectional fiber orientation over the entire length of the spring by an interposed spacer layer 3, which is composed of a fiber fabric or scrim, for example of the same material, but with a crosswise orientation of the fibers with respect to the unidirectional fiber strands of the cover layers 1, 2 or with respect to the longitudinal axis of the leaf spring.
  • the fiber orientation is ⁇ 45 °.
  • the spacer layer 3 should be able to absorb transverse and unilateral longitudinal forces, which lead to embrasure pressures in the bores 4 of spring connection lugs 3.1 of the spacer layer, it is of course also possible for fiber orientations to alternate ⁇ 45 ", 0" in a special application for this purpose. / 90 " ⁇ 45” etc. can be used or also in the case of fiber fabrics +60 “. -60 °, 0", 0 °, -60 ", + 60 ° depending on the load.
  • This spacer layer 3 is decisive for the spring thickness decreasing towards both ends of the spring, which is achieved, for example, by layering the fabric layers with different lengths.
  • the selected shape of the leaf spring or its spacer layer 3 has the advantage that approximately the same bending stresses over the spring length can be expected under spring deflection.
  • the spring provided in the middle can Bores 4 can also be designed open in the special application. So that unidirectional fiber strands are not severed by such connection bores created in the finished spring body only, i.e. the cover layers 1, 2 are not weakened, the bores 4 are limited to the uncovered areas of the spacer layer 3, which at the two longitudinal edges of the spring from the cover layers 1, 2 in Protrude the shape of the spring connection tabs 3.1. Due to the selected arrangement of the bores 4 exclusively in the intermediate layer optimized for this purpose, high forces occurring in the transverse or longitudinal direction of the spring can be transferred to the spring connection area. This is e.g. B. indispensable in motor vehicle construction, since the leaf spring must also take over wheel guiding forces.
  • a leaf spring of the type described above namely with side tabs 3.1, is not restricted to a spacer layer 3 of decreasing thickness.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Springs (AREA)

Description

Die Erfindung betrifft eine Biegefeder gemäß dem Oberbegriff des Patentanspruchs 1 und deren Herstellung.The invention relates to a spiral spring according to the preamble of claim 1 and its manufacture.

Bei einer derartigen durch die DE-C-1 231 967 bekannten Biegefeder werden die Federdicken- änderungen durch einen entsprechenden Faseraufbau der Abstandsschicht erreicht. Hierzu brauchen die Fasern der Abstandsschicht nicht unbedingt unidirektional orientiert zu sein, sondern können ebenso, entsprechend der durch die EP-A-5 916 bekannten Biegefeder, eine planlose Orientierung aufweisen. Schließlich wird der funktionale Zweck der Abstandsschicht, für gleiche Federspannungen in den Federdeckschichten über die gesamte Federlänge zu sorgen, gemäß der FR-A-1 411 011 auch durch Verwendung von Fasergewebe erreicht.In such a spiral spring known from DE-C-1 231 967, the spring thickness changes are achieved by a corresponding fiber structure of the spacer layer. For this purpose, the fibers of the spacer layer do not necessarily have to be unidirectionally oriented, but can also have a haphazard orientation, corresponding to the spiral spring known from EP-A-5 916. Finally, according to FR-A-1 411 011, the functional purpose of the spacer layer, to ensure equal spring tensions in the spring cover layers over the entire length of the spring, is also achieved by using fiber tissue.

Für sämtliche bekannten Ausführungsformen der Biegefeder besteht, unabhängig vom Faseraufbau und von der Form der Abstandsschicht, in der Federmitte das Problem der Krafteinleitung ohne Schwächung der Faserstränge der Deckschichten durch Bohrungen, sofern diese, etwa aus Gründen der Fertigungsvereinfachung, erst im fertigen Federgrundkörper geschaffen werden können. Hierbei geht es nicht nur um das Verhindern von Federbrüchen schlechthin. Vielmehr begünstigen solche, die Deckschichten durchdringenden, meist an den Federlängsrändern sitzenden Bohrungen Faserschäden, die an den betreffenden bei der Federdurchbiegung unter gleichzeitiger Torsion höchstbeanspruchten Stellen zu einer nach und nach fortschreitenden Biegefestigkeitsminderung führen. Diesem Problem läßt sich unter der im übrigen (natürlich) bestehenden Forderung nach größtmöglicher Verbindungssicherheit nicht schon durch einen mit der Biegefeder bloß verklemmten Beschlag beikommen.For all known embodiments of the spiral spring, regardless of the fiber structure and the shape of the spacer layer, there is the problem in the middle of the force application of force without weakening the fiber strands of the cover layers through holes, provided that these can only be created in the finished spring base body, for example for reasons of production simplification . This is not just about preventing feather breaks par excellence. Rather, such bores that penetrate the cover layers and usually sit on the longitudinal edges of the spring favor fiber damage, which lead to a gradually progressive reduction in bending strength at the relevant points that are subject to maximum stress during spring deflection with simultaneous torsion. This problem cannot be solved with the (naturally) existing demand for the greatest possible connection security by a fitting that is merely jammed with the spiral spring.

Der Erfindung liegt daher die Aufgabe zugrunde, bei einer Biegefeder der eingangs genannten Art erst im fertigen Federgrundkörper ohne Minderung der Festigkeit der Deckschichten Bohrungen für die Krafteinleitung einbringen zu können; im übrigen soll eine die Fertigung einer solchen Biegefeder vereinfachende Vorrichtung aufgezeigt werden.The invention is therefore based on the object, in the case of a spiral spring of the type mentioned, to be able to introduce bores for the application of force only in the finished spring base body without reducing the strength of the cover layers; moreover, a device which simplifies the production of such a spiral spring is to be shown.

Der erste Teil dieser Aufgabe ist gemäß dem Kennzeichen des Patentanspruchs 1 gelöst, also durch eine Möglichkeit zur Beschränkung von Federanschluß-Bohrungen auf die Abstandsschicht unter Strukturierung derselben derart, daß diese Bohrungen sich wesentlich weniger festigkeitsmindernd auswirken als bei Unidirektionalfaserstrukturen oder hiervon abweichenden Strukturen ohne bestimmte Faserorientierung. Denn die vorgeschlagene kreuzweise Faserorientierung erlaubt eine Belastung der Abstandsschicht sowohl durch die Längs- als auch durch in Querrichtung wirksame Kräfte. Damit können die auftretenden Lochleibungsdrücke von der Abstandsschicht optimal aufgenommen bzw. diese entsprechend ausgelegt werden.The first part of this task is solved according to the characterizing part of patent claim 1, i.e. by a possibility of restricting spring connection bores to the spacer layer while structuring the same in such a way that these bores have a much less strength-reducing effect than with unidirectional fiber structures or structures deviating therefrom without a specific fiber orientation . This is because the proposed crosswise fiber orientation allows the spacer layer to be stressed by both the longitudinal and transverse forces. In this way, the perforation reveal pressures that occur can be optimally absorbed by the spacer layer or they can be designed accordingly.

Der zweite Teil der vorgenannten Aufgabe ist durch ein Preßwerkzeug gemäß dem Patentanspruch 3 gelöst. Dieses hat nicht nur den Vorteil einer Einlegemöglichkeit für eine vorgeformte Abstandsschicht unter Sicherung derselben ge gen ein Verschieben beim Verpressen mit den (beispielsweise im Wickelverfahren im Preßwerkzeug herstellbaren) Deckschichten. Vielmehr läßt sich mit (im Unteranspruch 4 gekennzeichneten) einfachsten Maßnahmen sicherstellen, daß es beim Schließen des Preßwerkzeugs zu keiner Verschiebung von Fasersträngen in die Trennfugen zwischen den Wangenober- und Wangenunterteilen kommt. Damit ist eine in den jeweils gewünschten Abmessungen präzise Federfertigung gewährleistet.The second part of the above object is achieved by a press tool according to claim 3. This not only has the advantage of an insertion option for a preformed spacer layer while securing the same against displacement during pressing with the cover layers (which can be produced in the pressing tool, for example, by the winding method). Rather, the simplest measures (characterized in subclaim 4) ensure that there is no displacement of fiber strands into the joints between the upper and lower cheek parts when the pressing tool is closed. This ensures precise spring production in the dimensions required.

Die Erfindung wird nachfolgend anhand eines Ausführungsbeispiels weiter erläutert. Hierzu zeigt die Zeichnung in

  • Fig. 1 den Mittenabschnitt einer Blattfeder,
  • Fig. 2 bis 5 Verfahrensschritte bei der Fertigung einer Blattfeder gemäß Fig. 1, in Querschnittsdarstellung sämtlicher Teile.
The invention is further explained below using an exemplary embodiment. The drawing shows in
  • 1 shows the central section of a leaf spring,
  • Fig. 2 to 5 process steps in the manufacture of a leaf spring according to FIG. 1, in a cross-sectional view of all parts.

Die in Fig. 1 dargestellte gekrümmte Blattfeder mit von der Mitte zu beiden Enden hin abnehmender Dicke ist ein Schichtkörper aus Faserverbundwerkstoff. Hierbei sind zwei Deckschichten 1, 2 aus in einer Harz- oder dergleichen Bindungsmasse eingebetteten Glas- oder dergleichen Fasersträngen in unidirektionaler Faserorientierung über die gesamte Federlänge durch eine zwischengefügte Abstandsschicht 3 verbunden, welche aus einem Fasergewebe oder -gelege beispielsweise gleichen Materials aufgebaut ist, jedoch mit einer kreuzweisen Orientierung der Fasern gegenüber den Unidirektionalfasersträngen der Deckschichten 1, 2 bzw. in bezug auf die Blattfederlängsachse. Beispielsweise ist demgegenüber bei den dargestellten Faserstofflagen der Abstandsschicht 3 die Faserorientierung ±45°. Da die Abstandsschicht 3 quer- und einseitig auftretende Längskräfte, welche zu Lochleibungsdrücken in den Bohrungen 4 von Federanschluß-Laschen 3.1 der Abstandsschicht führen, aufnehmen können soll, kann für eine diesbezügliche Optimierung selbstverständlich im speziellen Anwendungsfall auch von Faserorientierungen abwechselnd ±45", 0"/90" ± 45" usw. Gebrauch gemacht werden oder auch im Falle von Fasergelegen +60". -60°, 0", 0°, -60", +60° je nach Lastfall.The curved leaf spring shown in Fig. 1 with a decreasing thickness from the center to both ends is a laminated body made of fiber composite material. Here, two cover layers 1, 2 of glass or similar fiber strands embedded in a resin or similar binding compound are connected in unidirectional fiber orientation over the entire length of the spring by an interposed spacer layer 3, which is composed of a fiber fabric or scrim, for example of the same material, but with a crosswise orientation of the fibers with respect to the unidirectional fiber strands of the cover layers 1, 2 or with respect to the longitudinal axis of the leaf spring. In contrast, for example, in the fiber layers of the spacer layer 3 shown, the fiber orientation is ± 45 °. Since the spacer layer 3 should be able to absorb transverse and unilateral longitudinal forces, which lead to embrasure pressures in the bores 4 of spring connection lugs 3.1 of the spacer layer, it is of course also possible for fiber orientations to alternate ± 45 ", 0" in a special application for this purpose. / 90 "± 45" etc. can be used or also in the case of fiber fabrics +60 ". -60 °, 0", 0 °, -60 ", + 60 ° depending on the load.

Diese Abstandsschicht 3 ist für die zu beiden Federenden hin abnehmende Federdicke maßgebend, was beispielsweise durch eine Schichtung der Gewebelagen mit unterschiedlicher Länge erreicht wird. Die gewählte Form der Blattfeder bzw. ihrer Abstandsschicht 3 hat den Vorteil, daß unter Federdurchbiegung mit annähernd gleichen Biegespannungen über die Federlänge gerechnet werden kann.This spacer layer 3 is decisive for the spring thickness decreasing towards both ends of the spring, which is achieved, for example, by layering the fabric layers with different lengths. The selected shape of the leaf spring or its spacer layer 3 has the advantage that approximately the same bending stresses over the spring length can be expected under spring deflection.

Für den Anschluß dieser Blattfeder, beispielsweise über einen Beschlag an einem Federträger, können die in der Federmitte vorgesehenen Bohrungen 4 im speziellen Anwendungsfall auch offen gestaltet sein. Damit durch solche erst im fertigen Federkörper geschaffene Anschlußbohrungen unidirektionale Faserstränge nicht durchtrennt, d. h., die Deckschichten 1, 2 nicht geschwächt werden, sind die Bohrungen 4 auf die unbedeckten Bereiche der Abstandsschicht 3 beschränkt, welche an den beiden Federlängsrändern aus den Deckschichten 1, 2 in Form der Federanschluß-Laschen 3.1 herausragen. Aufgrund der gewählten Anordnung der Bohrungen 4 ausschließlich in der dafür optimierten Zwischenschicht können hohe in Feder-Quer- oder Längsrichtung auftretende Kräfte in den Federanschlußbereich übergeleitet werden. Dies ist z. B. im Kfz-Bau unerläßlich, da hier die Blattfeder auch Radführungskräfte übernehmen muß.For the connection of this leaf spring, for example via a fitting on a spring support, the spring provided in the middle can Bores 4 can also be designed open in the special application. So that unidirectional fiber strands are not severed by such connection bores created in the finished spring body only, i.e. the cover layers 1, 2 are not weakened, the bores 4 are limited to the uncovered areas of the spacer layer 3, which at the two longitudinal edges of the spring from the cover layers 1, 2 in Protrude the shape of the spring connection tabs 3.1. Due to the selected arrangement of the bores 4 exclusively in the intermediate layer optimized for this purpose, high forces occurring in the transverse or longitudinal direction of the spring can be transferred to the spring connection area. This is e.g. B. indispensable in motor vehicle construction, since the leaf spring must also take over wheel guiding forces.

Selbstverständlich ist eine Blattfeder der vorbeschriebenen Art, nämlich mit seitlichen Laschen 3.1 nicht auf eine Abstandsschicht 3 abnehmender Dicke beschränkt.Of course, a leaf spring of the type described above, namely with side tabs 3.1, is not restricted to a spacer layer 3 of decreasing thickness.

Für die Fertigung dieser Blattfeder wird ein Preßwerkzeug bevorzugt, bei dem gemäß Fig. 5 eine Patrize 5 und eine Matrize 6 jeweils in Form eines auf einer Grundplatte 5.1 bzw. 6.1 sitzenden Stempels 5.2 bzw. 6.2 ausgebildet ist, welcher an seinen beiden Seitenflanken durch Seitenwangen 7 geführt wird; diese begrenzen die Breite der Blattfeder bzw. ihrer Schichten 1, 2, 3. Durch eine Profilierung der Seitenwangen 7 als jeweils längsgeteilte Fassungen der Federanschluß-Laschen 3.1 mit einem Wangenober- und einem Wangenunterteil 7.1 bzw. 7.2 ist erreicht, daß zum einen die Feder-Abstandsschicht 3 nach dem Schließen des Preßwerkzeugs gegen ein Verrutschen gesichert ist und daß zum anderen überhaupt erst der nachfolgend beschriebene problemlose Fertigungsablauf möglich wird:

  • Gemäß Fig. 2 werden zunächst zur Bildung der unteren Deckschicht 2 der Blattfeder auf der Grundplatte 6.1 der Matrize 6 die beiden Wangenunterteile 7.2 positioniert unter loser Zwischenfügung von Distanzstücken 8. Die Distanzstücke 8 haben jeweils eine solche Dicke, daß der durch den Matrizenstempel 6.2 und die Wangenunterteile 7.2 begrenzte Formraum bis zu der für die Abstandsschicht 3 bestimmten Auflagerfläche 7.2.1 am einzelnen Wangenunterteil eine solche Höhe aufweist, die zumindest der Dicke der unteren Deckschicht 2 einschließlich eines für das Pressen nötigen Materialzuschlages entspricht. Andernfalls würde es, bei der dargestellten nötigen Materialdicke, beim Einbringen der unidirektionalen Faserstränge für die untere Deckschicht 2 einer entsprechenden - in dem Maße praktisch nicht realisierbaren - Präzision der angewendeten Fasereinbringmethode bedürfen, damit beim Schließen des Preßwerkzeuges über die vorgenannten Auflagerflächen 7.2.1 hinaus aus dem Formraum keinerlei Faserstränge und Bindungsmasse derselben in die Fuge zwischen den Wangenober- und Wangenunterteilen 7.1 bzw. 7.2 fließen kann.
  • Gemäß Fig. 3 wird nach dem Einbringen der Faserstränge der unteren Deckschicht 2 die Abstandsschicht 3 aufgebracht, vorzugsweise als bereits gepreßter, formbeständiger Körper, der allerdings noch nicht ausgehärtet ist. Hiernach werden die beiden Wangenoberteile 7.1 positioniert. Die letzte Materialeinbringungsphase betrifft dann gemäß Fig. 4 die unidirektionalen Faserstränge der oberen Deckschicht 1 der Blattfeder. Schließlich wird das Preßwerkzeug durch Aufsetzen der Patrize 5 geschlossen. Die betreffende Fig. 5 zeigt, daß erst mit dem Schließen des Preßwerkzeuges die Distanzstücke 8 entfernt werden. Das anschließende Pressen durch Bewegen der Patrize 5 und Matrize 6 in den durch die Pfeile 9, 10 angegebenen Druckrichtungen kann in einer hydraulischen Presse erfolgen unter gleichzeitiger Zufuhr der für das gemeinsame Aushärten sämtlicher Schichten 1, 2, 3 nötigen Wärme. Es versteht sich, daß es hierbei nicht unbedingt zu einem Zusammenpressen der unidirektionalen Faserstränge um die Dicke der infolge der Distanzstücke 8 zwangsläufig zwischen der Matrize 6 und Patrize 5 einerseits und den Seitenwangen 7 andererseits vorhandenen Spalte 11 kommen muß, also diese bzw. die Distanzstücke ohne weiteres eine größere Dicke haben können, als der Preßschwund erfordert.
For the manufacture of this leaf spring, a pressing tool is preferred, in which, according to FIG. 5, a male 5 and a female 6 are each in the form of a plunger 5.2 or 6.2 seated on a base plate 5.1 or 6.1, which is provided on its two side flanks by side cheeks 7 is performed; these limit the width of the leaf spring or its layers 1, 2, 3. By profiling the side cheeks 7 as longitudinally divided versions of the spring connection tabs 3.1 with a cheek top and a cheek bottom 7.1 or 7.2 is achieved that on the one hand the spring Spacer layer 3 is secured against slipping after the pressing tool has been closed and that, on the other hand, the problem-free production process described below is only possible in the first place:
  • 2, the two lower cheek parts 7.2 are positioned with the loose interposition of spacers 8 to form the lower cover layer 2 of the leaf spring on the base plate 6.1 of the die 6. The spacers 8 each have a thickness such that the through the die stamp 6.2 and the Cheek lower parts 7.2 limited mold space up to the support surface 7.2.1 intended for the spacer layer 3 on the individual lower cheek part has a height which corresponds at least to the thickness of the lower cover layer 2 including a material surcharge required for the pressing. Otherwise, with the necessary material thickness shown, when introducing the unidirectional fiber strands for the lower cover layer 2, a corresponding - to an extent practically not feasible - precision of the fiber insertion method used would be required, so that when closing the pressing tool beyond the abovementioned support surfaces 7.2.1 no fiber strands and binding mass of the same can flow into the joint between the upper and lower cheek parts 7.1 and 7.2.
  • 3, after the introduction of the fiber strands of the lower cover layer 2, the spacer layer 3 is applied, preferably as an already pressed, dimensionally stable body which, however, has not yet hardened. The two upper cheek parts 7.1 are then positioned. According to FIG. 4, the last material introduction phase then relates to the unidirectional fiber strands of the upper cover layer 1 of the leaf spring. Finally, the pressing tool is closed by fitting the male 5. The relevant Fig. 5 shows that the spacers 8 are removed only when the pressing tool is closed. The subsequent pressing by moving the male 5 and female 6 in the pressure directions indicated by the arrows 9, 10 can take place in a hydraulic press with simultaneous supply of the heat necessary for the common hardening of all layers 1, 2, 3. It goes without saying that this does not necessarily mean that the unidirectional fiber strands have to be compressed by the thickness of the gaps 11 that are inevitably present between the die 6 and the patrix 5 on the one hand and the side cheeks 7 on the other hand due to the spacers 8, that is to say these or the spacers without can also have a greater thickness than the shrinkage required.

Claims (4)

1. A bending spring made from fibre-reinforced plastics material, more especially in the form of a curved leaf spring with a thickness which decreases from the centre towards both ends, in which fibre strands, in unidirectional fibre orientation over the spring length, form two surface layers (1, 2) of an intermediate layer (3) which is interpolated therebetween and is materially connected thereto and which consists of fibre fabric or the like, characterized in that the intermediate layer (3) juts out on both longitudinal edges of the spring from the surface layers (1, 2) in the form of a spring connection strap (3.1) and in that as compared with the fibre strands of the surface layers (1, 2) the fibres of the intermediate layer (3) are arranged in a predominantly crosswise orientation.
2. A bending spring according to claim 1, characterized in that spring connection bores (4) are restricted to the two spring connection straps (3.1).
3. A pressing tool consisting of upper die (5) and bottom die (6) for producing a bending spring according to claim 1, characterized in that the upper die (5) and bottom die (6) is in each case designed in the form of a die (5.2 or 6.2 respectively) seated on a base plate (5. 1 or 6.1 respectively), in which respect each die is guided at its two side flanks by side cheeks (7) which limit the surface and intermediate layer width and which are profiled in each case as longitudinally-split frames of the spring connection straps (3.1) with a cheek upper and a cheek lower part (7.1 or 7.2 respectively).
4. A pressing tool according to claim 3, characterized in that between the base plate (6.1) of the bottom die (6) and the cheek lower parts (7.2) are loosely inserted distance pieces (8) of at least such a thickness that a moulding chamber bounded by the female die (6.2) and the cheek lower parts (7.2) has, as far as a bearing surface (7.2.1) on the individual cheek lower part intended for the intermediate layer (3), a height which corresponds at least to the thickness of the lower surface layer (2) including a material increase necessary for the pressing.
EP82110755A 1981-12-18 1982-11-20 Flexible fibre-reinforced plastic spring and press for its manufacture Expired EP0082321B1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE3150162 1981-12-18
DE3150162 1981-12-18
DE3238099A DE3238099C2 (en) 1981-12-18 1982-10-14 Spiral spring made of fiber-reinforced plastic and pressing tool for their manufacture
DE3238099 1982-10-14

Publications (3)

Publication Number Publication Date
EP0082321A2 EP0082321A2 (en) 1983-06-29
EP0082321A3 EP0082321A3 (en) 1983-11-30
EP0082321B1 true EP0082321B1 (en) 1985-09-11

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Application Number Title Priority Date Filing Date
EP82110755A Expired EP0082321B1 (en) 1981-12-18 1982-11-20 Flexible fibre-reinforced plastic spring and press for its manufacture

Country Status (2)

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EP (1) EP0082321B1 (en)
DE (1) DE3238099C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103415722A (en) * 2011-03-10 2013-11-27 日本发条株式会社 Fiber reinforced plastic spring

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3243519A1 (en) * 1982-11-25 1984-05-30 Basf Ag, 6700 Ludwigshafen METHOD FOR THE PRODUCTION OF SPRING RODS FROM FIBER COMPOSITE MATERIALS
JPS59101359A (en) * 1982-12-02 1984-06-11 日本発条株式会社 Fiber reinforced plastic board and its manufacture
GB8306653D0 (en) * 1983-03-10 1983-04-13 Secr Defence Fibre reinforced composites
US4772044A (en) * 1983-08-22 1988-09-20 Booher Benjamin V Vehicle suspension system with flexible control arm
US4509774A (en) * 1983-08-22 1985-04-09 Booher Benjamin V Composite control arm apparatus
US4613152A (en) * 1985-05-01 1986-09-23 Booher Benjamin V Composite transverse beam and spring system for an automobile
US4676488A (en) * 1986-01-08 1987-06-30 American Motors Corporation Tapered leaf spring
DE3722893C1 (en) * 1987-07-10 1988-06-09 Messerschmitt Boelkow Blohm Spring with spiral spring arms
FR2654975B1 (en) * 1989-11-24 1992-03-27 Vollet Jerome PROCESS FOR MOLDING A PART OF A COMPOSITE MATERIAL.
DE10153875A1 (en) * 2001-11-02 2003-05-15 Bpw Bergische Achsen Kg Component in an elongated construction made of a fiber-plastic composite
DE10241009A1 (en) * 2002-09-05 2004-03-25 Bombardier Transportation Gmbh Device for clamping fiber composite components
DE102005055049B4 (en) * 2005-11-16 2013-06-20 Ifc Composite Gmbh Process for producing a leaf spring made of a fiber composite material
KR101602388B1 (en) * 2011-09-15 2016-03-10 가부시키가이샤 지에이치 크래프트 Flat spring for railroad vehicle bogie
DE102014110558A1 (en) * 2014-07-25 2016-01-28 Tobias KELLER Biegefederelement of a fiber-reinforced plastic composite material

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1411011A (en) * 1963-07-24 1965-09-17 Fairey Sa Springs and their manufacturing process
EP0005916A1 (en) * 1978-05-26 1979-12-12 GKN Group Services Limited Spring manufacture

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB230679A (en) * 1924-06-04 1925-03-19 Walter Murdoch Improved means for reducing the risk of breakage in laminated springs for road vehicles
DE939733C (en) * 1953-05-09 1956-03-01 Daimler Benz Ag Leaf suspension for motor vehicles
FR1100286A (en) * 1953-05-09 1955-09-19 Daimler Benz Ag Leaf elastic suspension device for motor cars
DE1231967B (en) * 1963-05-30 1967-01-05 Sachsenring Automobilwerke Glass fiber synthetic resin spring, especially for motor vehicles
US3968958A (en) * 1972-11-30 1976-07-13 Edgewater Corporation Composite material springs and manufacture
JPS602540B2 (en) * 1977-11-25 1985-01-22 東レ株式会社 composite leaf spring
JPS5814934B2 (en) * 1978-10-19 1983-03-23 東邦ベスロン株式会社 Leaf spring and its manufacturing method

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1411011A (en) * 1963-07-24 1965-09-17 Fairey Sa Springs and their manufacturing process
EP0005916A1 (en) * 1978-05-26 1979-12-12 GKN Group Services Limited Spring manufacture

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103415722A (en) * 2011-03-10 2013-11-27 日本发条株式会社 Fiber reinforced plastic spring

Also Published As

Publication number Publication date
DE3238099C2 (en) 1983-11-17
EP0082321A2 (en) 1983-06-29
DE3238099A1 (en) 1983-07-14
EP0082321A3 (en) 1983-11-30

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